CN205738070U - There is the unmanned plane of thrust line variset - Google Patents
There is the unmanned plane of thrust line variset Download PDFInfo
- Publication number
- CN205738070U CN205738070U CN201620414883.5U CN201620414883U CN205738070U CN 205738070 U CN205738070 U CN 205738070U CN 201620414883 U CN201620414883 U CN 201620414883U CN 205738070 U CN205738070 U CN 205738070U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- variset
- propeller
- thrust line
- frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn - After Issue
Links
Abstract
The utility model discloses a kind of unmanned plane with thrust line variset; belong to a kind of civilian unmanned plane; including fuselage; fuselage is provided with multiple frame; propeller it is designed with in frame; being mounted on multiple fixing bar in each frame, the end of multiple fixing bars is provided with oar guard circle, oar guard circle is placed in the outside of propeller；Propeller is all arranged in respective frame by thrust line variset；By setting up the oar guard circle being placed in outside propeller in frame; the rotation of exotic interference propeller during unmanned plane during flying can be avoided as far as possible; and by setting up thrust line variset between propeller power motor and frame, the recoil that stability when being effectively improved unmanned plane during flying and emitter produce when launching；Simple in construction the most of the present utility model, can by control end to the speed of unmanned plane during flying, highly, the state of position and The Cloud Terrace discharger be controlled, solve the compatibility issue of purposes equipment in every profession and trade, range of application is wide.
Description
Technical field
This utility model relates to a kind of civilian unmanned plane, and in particular, this utility model relates generally to a kind of unmanned plane with thrust line variset.
Background technology
Existing unmanned air vehicle technique defect is the demand different according to user, the transformation of the different size that unmanned plane is to be reached, and improved unmanned plane cost is higher, and does not has the breakthrough on practical significance on technological layer.And the shortcoming that unmanned plane is maximum at present is exactly the flying power of battery, the equipment carry of different industries technical field focuses with compatibility, the poor stability flown, the photographic head of lift-launch in addition, it is impossible to zoom stabilization shoots；In the rain, sea cannot preferably prevent fuselage waterproof with camera apparatus etc..And due to the defect of battery durable ability, loading capacity is directly proportional with flying power, it is impossible to often the time scouts, and major part The Cloud Terrace carry equipment is incompatible with unmanned plane itself；Ye You producer goes to transform the structure of unmanned plane according to customer demand the most on the market, the fields such as such as agriculture, mapping, fire prevention scouting, though this kind of improved unmanned plane meets the demand of user, but it is the most relatively costly, it is unfavorable for large-scale popularization and application, thus is necessary very existing unmanned plane structure to be studied and improved.
Utility model content
One of the purpose of this utility model is for above-mentioned deficiency, a kind of unmanned plane with thrust line variset is provided, solving unmanned plane during flying poor stability in prior art with expectation, carrying equipment compatibility is not enough, and flight is vulnerable to the technical problems such as the interference of exotic.
For solving above-mentioned technical problem, this utility model by the following technical solutions:
A kind of unmanned plane with thrust line variset provided by the utility model; including fuselage; described fuselage is provided with multiple frame; it is designed with propeller in each frame; multiple fixing bar it is mounted in described each frame; being provided with oar guard circle on the end of the plurality of fixing bar, described oar guard circle is placed in the outside of propeller；Described propeller is all arranged in respective frame by thrust line variset, and described thrust line variset includes X-axis module and Z axis module, and described Z axis module activities is arranged in X-axis module, and X-axis module activities is arranged in frame；Being mounted on respective power motor in the Z axis module of thrust line variset, the output shaft of described power motor is connected with propeller power, for being driven propeller to rotate in oar guard circle by power motor；Being also equipped with The Cloud Terrace discharger on described fuselage, described The Cloud Terrace discharger includes that The Cloud Terrace support and emitter, described The Cloud Terrace support are arranged on fuselage by rotary shaft, and described emitter is arranged in The Cloud Terrace support by pitch axis；Described rotary shaft is all connected with respective driving motor power with pitch axis.
As preferably, further technical scheme is: be additionally provided with trigger on described emitter, and described trigger is connected with servo-driver power by connecting rod, for being driven startup trigger by servo-driver by connecting rod, makes emitter launch its internal utensil.
Further technical scheme is: described The Cloud Terrace support is arranged on the bottom of fuselage by rotary shaft.
Further technical scheme is: be also equipped with miniature camera or minicam on described emitter.
Further technical scheme is: be also equipped with miniature camera or minicam on described fuselage.
Further technical scheme is: the front end of described fuselage is additionally provided with vision and ultrasonic system, described vision and ultrasonic system at least include binocular vision sensor and ultrasonic sensor, described binocular vision sensor and ultrasonic sensor equal Access Control module, described control module also access communications module, for being detected the barrier in current flight environment by control module by binocular vision sensor and ultrasonic sensor, regenerate flight path according to the position of barrier；And the unmanned plane positional information determined according to binocular vision sensor and ultrasonic sensor is transmitted to controlling end by communication module by control module.
Further technical scheme is: described miniature camera or minicam also Access Control module, transmits to controlling end for real-time image information miniature camera or minicam collected by communication module by control module.
Further technical scheme is: described servo-driver, power motor, driving motor equal Access Control module, for being received the control information controlling end by communication module by control module, and control servo-driver, power motor, driving motor perform the operation corresponding with described control information.
Further technical scheme is: the plurality of fixing bar is placed in the lower section of propeller.
Further technical scheme is: the material of described fuselage, frame, oar guard circle, propeller and The Cloud Terrace support is carbon fiber board.
Compared with prior art; one of the beneficial effects of the utility model are: by setting up the oar guard circle being placed in outside propeller in frame; the rotation of exotic interference propeller during unmanned plane during flying can be avoided as far as possible; and by setting up thrust line variset between propeller power motor and frame, the recoil that stability when being effectively improved unmanned plane during flying and emitter produce when launching；And by the The Cloud Terrace support also adjustable transmitter on fuselage or the real time position of video camera, it is ensured that also can improve the jitter problem of video camera shooting after the accuracy of video camera shooting, and stability lifting；A kind of unmanned plane simple in construction with thrust line variset the most provided by the utility model, can by control end to the speed of unmanned plane during flying, highly, the state of position and The Cloud Terrace discharger is controlled, more press close to industry requirement, solving the compatibility issue of purposes equipment in every profession and trade, range of application is wide.
Accompanying drawing explanation
Fig. 1 is the structural representation for one embodiment of this utility model is described；
Fig. 2 is for oar guard circle and the structural representation of fixing bar in one embodiment of this utility model are described；
Fig. 3 is for the thrust line variset structural representation in one embodiment of this utility model is described；
Fig. 4 is for the The Cloud Terrace discharger structural representation in one embodiment of this utility model is described；
Fig. 5 is for the vision in another embodiment of this utility model and ultrasonic system structural representation are described；
In figure, 1 it is fuselage, 2 is frame, 3 is propeller, 4 is fixing bar, 5 is oar guard circle, 6 is thrust line variset, 61 is X-axis module, 62 is Z axis module, 7 is The Cloud Terrace discharger, 71 is The Cloud Terrace support, 72 is emitter, 8 is rotary shaft, 9 is pitch axis, 10 is trigger, 11 is connecting rod, 12 is servo-driver, 13 is vision and ultrasonic system.
Detailed description of the invention
Below in conjunction with the accompanying drawings this utility model is further elaborated.
With reference to shown in Fig. 1; an embodiment of the present utility model is a kind of unmanned plane with thrust line variset; including fuselage 1; it is provided with multiple frame 2 on the fuselage 1; quantity about frame; inventor is with reference to prior art; think that being preferably set to four shown in figure is advisable; it is designed with propeller 3 in each frame 2; what is more important, each frame 2 is mounted on multiple fixing bar 4, the end of multiple fixing bars 4 is provided with oar guard circle 5; going out as shown in Figure 2, oar guard circle 5 is placed in the outside of propeller 3；And the radius of this oar guard circle 5 need to be slightly larger than the blade length of propeller 3, it is preferred that multiple fixing bars 4 are preferably disposed in the lower section of propeller 3, rotate avoiding interference propeller 3；
With reference to shown in Fig. 3, with prior art except that, aforesaid propeller 3 is all arranged in respective frame 2 by thrust line variset 6, this thrust line variset 6 includes X-axis module 61 and Z axis module 62, Z axis module 62 is movably arranged in X-axis module 61, then X-axis module 61 is movably arranged in frame 2；And in the Z axis module 62 of thrust line variset 6, it is both needed to install respective power motor; the axis power of the output shaft of this power motor with above-mentioned propeller 3 is connected; for being driven propeller 3 to rotate in oar guard circle 5 by power motor, and then generation air-flow makes unmanned plane during flying；
X-axis module 61 in above-mentioned thrust line variset 6 plays the effect that the power motor when unmanned plane during flying carries out rotating around X-axis；Z axis module 62 plays the effect that the power motor when unmanned plane during flying carries out rotating about the z axis；And then the stability during unmanned plane during flying and motility can be greatly reinforced, at different landform and weather in-flight, by changing motor and the angle of inclination of propeller, fuselage can be kept farthest stable；Making unmanned plane pulling force dynamics of taking off bigger, speed faster, makes unmanned plane carry out flare maneuver, flexible movements by the way of changing air-flow, and cruising time is the biggest simultaneously.
Shown in Fig. 4, on above-mentioned fuselage 1, The Cloud Terrace discharger 7 is also installed again, this The Cloud Terrace discharger 7 includes The Cloud Terrace support 71 and emitter 72, and this The Cloud Terrace support 71 is installed on the fuselage 1 by rotary shaft 8, and emitter 72 is arranged in The Cloud Terrace support 71 by pitch axis 9；And rotary shaft 8 is all connected with respective driving motor power with pitch axis 9；And then by rotary shaft 8 and the pitch axis 9 i.e. real-time angular of adjustable transmitter 72, it is ensured that unmanned plane is launched or the accuracy of shooting；Preferably technological means is herein, and aforementioned The Cloud Terrace support 71 can be arranged on the bottom of fuselage 1 by rotary shaft 8.
In the present embodiment; by setting up the oar guard circle 5 being placed in outside propeller in frame 2; the rotation of exotic interference propeller 3 during unmanned plane during flying can be avoided as far as possible; and by setting up thrust line variset 6 between propeller 3 power motor and frame 2, the recoil that stability when being effectively improved unmanned plane during flying and emitter 72 produce when launching；And by the The Cloud Terrace support 71 also adjustable transmitter on fuselage 1 or the real time position of video camera, it is ensured that also can improve the jitter problem of video camera shooting after the accuracy of video camera shooting, and stability lifting.
Based on the above embodiments, above-mentioned The Cloud Terrace discharger 7 has also been done further improvement by inventor, to facilitate control, the most as shown in Figure 4, trigger 10 set up by above-mentioned emitter 72, this trigger 10 is connected with servo-driver 12 power by connecting rod 11, for being driven startup trigger 10 by servo-driver 12 by connecting rod 11, emitter 72 is made to launch its internal utensil, this utensil can load such as equipment and patterns such as firefighting cartridge, howitzer, flare pistol, earth station's fixed points at emitter 72 according to different demands；
In the present embodiment, directly can install miniature camera or minicam on emitter 72, with the demand of satisfied shooting, the shooting angle of miniature camera or minicam is consistent with the angle of emitter 72 simultaneously.In addition, fuselage 1 itself also can be as a The Cloud Terrace installing capture apparatus, and the most aforesaid miniature camera or minicam also can be directly mounted on fuselage 1.
With reference to shown in Fig. 1 Yu Fig. 5, at this utility model for solving in a technical problem embodiment more preferably, for the ease of operator, unmanned plane is controlled, front end at fuselage 1 can set up vision and ultrasonic system 13 again, this vision and ultrasonic system 13 at least include binocular vision sensor and ultrasonic sensor, binocular vision sensor and ultrasonic sensor are all accessed the control module within unmanned plane, control module also access communications module, for being detected the barrier in current flight environment by control module by binocular vision sensor and ultrasonic sensor, position according to barrier regenerates flight path；And the unmanned plane positional information determined according to binocular vision sensor and ultrasonic sensor is transmitted to controlling end by communication module by control module；Aforesaid control module can use the control chips such as CPU, MCU, and the wireless signal such as the used infrared ray of communication module, 3G, 4G, GPRS, Wifi is transmitted；It is said that in general, vision and ultrasonic system 13 start when flying height is less than 10 meters, hovering precision and flight stability can be strengthened.Even if indoor etc. without in the environment of gps signal, unmanned plane also can smooth flight.
In the present embodiment, above-mentioned miniature camera or minicam also need Access Control module, transmit to controlling end for real-time image information miniature camera or minicam collected by communication module by control module；As be inconvenient to transmit, also can directly image information be stored in the storage medium in miniature camera or minicam.
Further, above-mentioned servo-driver 12, power motor, driving motor need equal Access Control module, for being received the control information controlling end by communication module by control module, and control servo-driver 12, power motor, driving motor perform the operation corresponding with described control information.
Based on this utility model the above embodiments; inventor is in view of the flying power of unmanned plane; the power motor of propeller 3 and the material of unmanned plane itself are studied; it is specially and uses carbon fiber version to be processed into above-mentioned fuselage 1, frame 2, oar guard circle 5, propeller 3 and The Cloud Terrace support 71; thus reduce the weight that unmanned plane is overall, and prevent from getting rusty；
The most also the problem of power motor is optimized, the unmanned plane specially varied in weight and equipment thereof use the power motor of different size to go collocation, allow the more stable flight of unmanned plane, the configuration of power motor also requires, also it is related with stability due to power motor, and the carry weight of unmanned plane also will have influence on degree of having a smooth flight, therefore power motor improves collocation with blade must improve, the propeller 3 producing motor configuration needs through counterweight to debug unmanned plane, and test of many times to be passed through goes to measure power motor vulnerability degree with persistence.The i.e. specification of power motor is to design in strict accordance with unmanned plane counterweight, needs according to size of current, and the specification of accessory produces；The size of electric current directly influences unmanned plane powerup issue, produces more unnecessary consequence；Therefore in power motor specification produces, it is also necessary to going configuration according to the requirement of design with parameter, interface is with on weight will match various unmanned plane equipment.
Unmanned plane parameter employed in the above-mentioned preferred embodiment of this utility model is as follows:
Fuselage overall weight 1000g～2500g
Frame wheelbase: 1000mm
Propeller size: 28 cun of (2880) noises are little
The parameter of electric machine: U8 waterproof machine
Electricity adjusts parameter: 80A electricity is adjusted
Battery parameter: 6s 22000mah is full of voltage 25.2v or 26.1v(high-tension battery) 2500g
Wind loading rating: 5-7 level
The equipment of fuselage loading capacity, overweight more than 500G can be met by carry, can shorten cruising time；
On the other hand, fuselage 1 inside center plate (or panel) can design according to water resistance, most of electric wire of unmanned plane, and GPS is an exposure to outward, by this design, allow industry user's technology preferably transform water proof equipment carry with power module etc..
Than that described above, this utility model also has a characteristic that based on the unmanned plane with thrust line variset described by above-described embodiment
1) contrasting existing technology, unmanned plane civil nature is extensive, and this utility model, by improving with perfect, is researched and developed according to industry requirement, more can press close to industry requirement, the most preferably solve the compatibility of industrial applications equipment.
2) unmanned plane researched and developed by Amazon is contrasted, and the unmanned plane of Amazon design is automatic delivery perfect in shape and function, embodies more intelligent development, preferably saves the artificial time.Of the present utility model is also the demand for industry user, meet the demand of more users with innovation idea, by the later stage to the compatibility of earth station with using, compare region widely in safety, the automatic delivery function as Amazon unmanned plane is similar to (the domestic difference owing to building is not appropriate for this functionality) can be met.
3) unmanned plane is presently required the problem of solution has any to be not fee from noise problem, and today extensively used of civilian unmanned plane, military unmanned air vehicle receives much concern the most always, but military unmanned air vehicle must solve noise problem.U.S. Military unmanned plane has research and development noise elimination unmanned plane really, price is also strictly nobody and can accept, it is multi-purpose unmanned aerial vehicle since provided by the utility model, power motor problem is also carried out improve, for the unmanned plane motor noise of other brands, really it has been little much on noise, the most more can press close to military use.
Than that described above, it can further be stated that " embodiment ", " another embodiment ", " embodiment " spoken of in this manual etc., the specific features, structure or the feature that refer to combine the description of this embodiment are included at least one embodiment that the application generality describes.The most multiple local appearance statement of the same race is not necessarily to refer to same embodiment.Furthermore, it is understood that combine any embodiment when describing a specific features, structure or feature, to be advocated is to combine other embodiments also to fall in the range of this utility model to realize this feature, structure or feature.
This utility model is described by multiple explanatory embodiment the most of the present utility model, but, should be appreciated that, those skilled in the art can be designed that a lot of other amendments and embodiment, and these amendments and embodiment will fall within spirit disclosed in the present application and spirit.More specifically, in the range of disclosure, drawings and claims, the building block of theme composite configuration and/or layout can be carried out multiple modification and improvement.In addition to the modification carrying out building block and/or layout and improvement, to those skilled in the art, other purposes also will be apparent from.
Claims (10)
1. a unmanned plane with thrust line variset; including fuselage (1); described fuselage (1) is provided with multiple frame (2); propeller (3) it is designed with in each frame (2); it is characterized in that: on described each frame (2), be mounted on multiple fixing bar (4); being provided with oar guard circle (5) on the end of the plurality of fixing bar (4), described oar guard circle (5) is placed in the outside of propeller (3)；
Described propeller (3) is all arranged in respective frame (2) by thrust line variset (6), described thrust line variset (6) includes X-axis module (61) and Z axis module (62), described Z axis module (62) is movably arranged in X-axis module (61), and X-axis module (61) is movably arranged in frame (2)；Being mounted on respective power motor in the Z axis module (62) of described thrust line variset (6), the output shaft of described power motor is connected with propeller (3) power, for being driven propeller (3) to rotate in oar guard circle (5) by power motor；
The Cloud Terrace discharger (7) it is also equipped with on described fuselage (1), described The Cloud Terrace discharger (7) includes The Cloud Terrace support (71) and emitter (72), described The Cloud Terrace support (71) is arranged on fuselage (1) by rotary shaft (8), and described emitter (72) is arranged in The Cloud Terrace support (71) by pitch axis (9)；Described rotary shaft (8) is all connected with respective driving motor power with pitch axis (9).
The unmanned plane with thrust line variset the most according to claim 1, it is characterized in that: on described emitter (72), be additionally provided with trigger (10), described trigger (10) is connected with servo-driver (12) power by connecting rod (11), for being driven startup trigger (10) by servo-driver (12) by connecting rod (11), emitter (72) is made to launch its internal utensil.
The unmanned plane with thrust line variset the most according to claim 2, it is characterised in that: described The Cloud Terrace support (71) is arranged on the bottom of fuselage (1) by rotary shaft (8).
The unmanned plane with thrust line variset the most according to claim 1, it is characterised in that: described emitter is also equipped with miniature camera or minicam on (72).
The unmanned plane with thrust line variset the most according to claim 1, it is characterised in that: described fuselage is also equipped with miniature camera or minicam on (1).
6. according to the unmanned plane with thrust line variset described in claim 4 or 5, it is characterized in that: the front end of described fuselage (1) is additionally provided with vision and ultrasonic system (13), described vision and ultrasonic system (13) at least include binocular vision sensor and ultrasonic sensor, described binocular vision sensor and ultrasonic sensor equal Access Control module, described control module also access communications module, for being detected the barrier in current flight environment by control module by binocular vision sensor and ultrasonic sensor, position according to barrier regenerates flight path；And the unmanned plane positional information determined according to binocular vision sensor and ultrasonic sensor is transmitted to controlling end by communication module by control module.
The unmanned plane with thrust line variset the most according to claim 6, it is characterized in that: described miniature camera or minicam also Access Control module, transmit to controlling end for the real-time image information by communication module, miniature camera or minicam collected by control module.
The unmanned plane with thrust line variset the most according to claim 2, it is characterized in that: described servo-driver (12), power motor, driving motor equal Access Control module, for being received the control information controlling end by communication module by control module, and control servo-driver (12), power motor, driving motor perform the operation corresponding with described control information.
The unmanned plane with thrust line variset the most according to claim 1, it is characterised in that: the plurality of fixing bar (4) is placed in the lower section of propeller (3).
The unmanned plane with thrust line variset the most according to claim 1, it is characterised in that: the material of described fuselage (1), frame (2), oar guard circle (5), propeller (3) and The Cloud Terrace support (71) is carbon fiber board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414883.5U CN205738070U (en) | 2016-05-10 | 2016-05-10 | There is the unmanned plane of thrust line variset |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620414883.5U CN205738070U (en) | 2016-05-10 | 2016-05-10 | There is the unmanned plane of thrust line variset |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205738070U true CN205738070U (en) | 2016-11-30 |
Family
ID=57371379
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620414883.5U Withdrawn - After Issue CN205738070U (en) | 2016-05-10 | 2016-05-10 | There is the unmanned plane of thrust line variset |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205738070U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105905286A (en) * | 2016-05-10 | 2016-08-31 | 深圳市旋翼捷科技有限公司 | Unmanned aerial vehicle with thrust line variable device |
| CN107176298A (en) * | 2017-05-28 | 2017-09-19 | 珠海磐磊智能科技有限公司 | Aircraft flight control method and aircraft |
| CN107907889A (en) * | 2017-12-25 | 2018-04-13 | 成都壹橙科技有限公司 | A kind of deliverance apparatus based on unmanned plane |
| CN109436313A (en) * | 2018-12-21 | 2019-03-08 | 辽宁壮龙无人机科技有限公司 | Multi-rotor unmanned aerial vehicle |
-
2016
- 2016-05-10 CN CN201620414883.5U patent/CN205738070U/en not_active Withdrawn - After Issue
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105905286A (en) * | 2016-05-10 | 2016-08-31 | 深圳市旋翼捷科技有限公司 | Unmanned aerial vehicle with thrust line variable device |
| CN105905286B (en) * | 2016-05-10 | 2018-02-27 | 深圳市旋翼捷科技有限公司 | Unmanned plane with thrust line variset |
| CN107176298A (en) * | 2017-05-28 | 2017-09-19 | 珠海磐磊智能科技有限公司 | Aircraft flight control method and aircraft |
| CN107176298B (en) * | 2017-05-28 | 2020-01-03 | 珠海磐磊智能科技有限公司 | Aircraft flight control method and aircraft |
| CN107907889A (en) * | 2017-12-25 | 2018-04-13 | 成都壹橙科技有限公司 | A kind of deliverance apparatus based on unmanned plane |
| CN109436313A (en) * | 2018-12-21 | 2019-03-08 | 辽宁壮龙无人机科技有限公司 | Multi-rotor unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105905286A (en) | Unmanned aerial vehicle with thrust line variable device | |
| CN205738070U (en) | There is the unmanned plane of thrust line variset | |
| US9493235B2 (en) | Amphibious vertical takeoff and landing unmanned device | |
| CN107087427B (en) | Control method, device and the equipment and aircraft of aircraft | |
| CN205263655U (en) | A system, Unmanned vehicles and ground satellite station for automatic generation panoramic photograph | |
| US9456185B2 (en) | Helicopter | |
| CN105045279A (en) | System and method for automatically generating panorama photographs through aerial photography of unmanned aerial aircraft | |
| CN104808680A (en) | Multi-rotor flight shooting device | |
| CN101811578A (en) | Special photoelectric nacelle of power patrol unmanned helicopter | |
| CN106471337A (en) | Interchangeable mounting platform | |
| CN110347171A (en) | A kind of flying vehicles control method and aircraft | |
| CN202600486U (en) | Aerial remote sensing platform airborne operation control system | |
| CN105242685A (en) | Unmanned plane flight accompanying aerial photographing system and method | |
| CN206532142U (en) | A kind of rotor wing unmanned aerial vehicle tenacious tracking of view-based access control model moves the control system of target | |
| CN205015741U (en) | Companion flies unmanned aerial vehicle system of taking photo by plane and control cabinet and unmanned aerial vehicle thereof | |
| CN106586009A (en) | Unmanned aerial vehicle | |
| CN106231191A (en) | Full-automatic aerial panoramic view data acquisition system, method and control terminal | |
| CN110488850A (en) | A kind of quadrotor drone vision navigation system and method based on raspberry pie | |
| CN104085529A (en) | Eight-rotor-wing unmanned plane system | |
| CN105292477A (en) | Wrist type portable accompanying flight autonomous supervision unmanned aerial vehicle | |
| CN105468029A (en) | Unmanned aerial vehicle aerial shooting device and unmanned aerial vehicle aerial shooting method | |
| CN104995575A (en) | Method and device of data processing and aircraft | |
| CN106742005A (en) | A kind of power-line patrolling photoelectric nacelle and depopulated helicopter | |
| CN207319073U (en) | Unmanned plane and unmanned flight's system | |
| CN204287973U (en) | flight camera |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20161130 Effective date of abandoning: 20180227 |
|
| AV01 | Patent right actively abandoned |